The invention discloses an unmanned aerial vehicle and a control method, the unmanned aerial vehicle comprises a fuselage and a flight control system arranged in the fuselage, wings are vertically arranged at the rear end of the fuselage, an engine and a fuel system for providing fuel for the engine are arranged below the wings, and the engine is connected with a propeller for providing thrust; a canard and a control mechanism used for controlling the canard to rotate are vertically arranged at the front end of the fuselage, motors and rotors mounted on the motors and used for providing thrust and lift force are fixed to the two ends of the canard, and the rotation directions of the rotors at the two ends of the canard are opposite. The height of the propeller is higher than that of the rotor wing; the control mechanism, the fuel system, the engine and the motor are all electrically connected to the flight control system. The structure of the wings and the canards is adopted, power is provided based on oil-electricity hybrid, and the system weight, the aerodynamic characteristics, the voyage and the endurance are considered.

    本发明公开了一种无人机及控制方法,包括机身和置于所述机身内的飞控系统,所述机身的后端垂直设置有机翼,所述机翼下方设置有发动机机和为所述发动机提供燃油供给的燃油系统,所述发动机上连接有用于提供推力的螺旋桨;所述机身的前端垂直设置有鸭翼和用于控制所述鸭翼转动的控制机构,所述鸭翼两端固定有电机和安装在电机上且用于提供推力和升力的旋翼,所述鸭翼两端的旋翼转动方向相反,该无人机在静止状态时,所述螺旋桨的高度高于所述旋翼的高度;所述控制机构、燃油系统、发动机和所述电机均电性连接于所述飞控系统。采用机翼和鸭翼的结构并基于油电混合提供动力,兼顾了系统重量、气动特性与航程、航时。


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    Titel :

    Unmanned aerial vehicle and control method


    Weitere Titelangaben:

    一种无人机及控制方法


    Beteiligte:
    WANG XU (Autor:in) / TIAN YUAN (Autor:in) / YAN XIANGFENG (Autor:in) / FENG CHENGLONG (Autor:in) / LI ZHIYI (Autor:in)

    Erscheinungsdatum :

    2024-05-14


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U